Function | Experimental rocket |
---|---|
Manufacturer | ONERA |
Country of origin | France |
Size | |
Height | 8.4 m (28 ft) |
Diameter | 0.4 m (1 ft 4 in) |
Mass | 1,000 kg (2,200 lb) |
Stages | 3 |
Associated rockets | |
Derivative work | Jericho (missile) |
Launch history | |
Status | Retired |
Launch sites | CERES - Ile de Levant |
Total launches | 3 |
Success(es) | 3 |
First stage – SPRAN-50 | |
Height | 2.5 m (8 ft 2 in) |
Diameter | 0.4 m (1 ft 4 in) |
Gross mass | 400 kg (880 lb) |
Burn time | 5.6 s |
Second stage –Jericho | |
Third stage –Melanie | |
Height | 1.60 m (5 ft 3 in) |
Diameter | 0.16 m (6.3 in) |
Empty mass | 10 kg (22 lb) |
Gross mass | 32 kg (71 lb) |
Propellant mass | 22 kg (49 lb) |
Maximum thrust | 11.10 kN (2,500 lbf) |
Specific impulse | 227 seconds (2.23 km/s) |
Burn time | 4.4 s |
Propellant | Solid |
Daniel (OPD-220-ADX) is the designation for a French experimental rocket,a precursor to the Israeli Jericho ballistic missile. [1] [2]
It consisted of 3 stages:a SPRAN-50 first stage,a Jericho second stage and a Mélanie third stage. [3] Daniel was capable of reaching a maximum altitude of 130 km and had a takeoff weight of 1000 kg,a diameter of 0.40 m and a length of 8.40 m [1]
Daniel was launched three times between 1959 and 1961 by ONERA from Centre d'Essais et de Recherches d'Engins Speciaux - Ile de Levant. [4] [2]
Date | Mission | Apogee |
---|---|---|
1959 January 27 | Atmosphere radioactivity | 127 km (78 mi) |
1961 October 5 | Test / aeronomy mission | 130 km (80 mi) |
1961 October 9 | Test / aeronomy mission | 130 km (80 mi) |
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